VNE (S.L.)

311

km/h

168

kts

Max cruise speed (S.L.)

285

km/h

154

kts

Rate of climb (S.L.)

9.8

m/sec

1930

ft/min

Hovering IGE

5060

m

16600

ft

Hovering OGE

3597

m

11800

ft

Service ceiling

5974

m

19600

ft

OEI max service ceiling

3993

m

13100

ft

Max Range (1)

965

km

521

NM

Max endurance (1)

5 h 04 min

†

(1) with 230 USGal fuel, no reserve, @5000 ft.

Max take Off (int./ loads)

2850

kg

6283

lb

Max take Off (ext./ loads)

3000

kg

6614

lb

Basic Empty Weights

1570

kg

3461

lb

Engine Rating (2 x Pratt & Whitney PW206C)

Take Off power (5 min)

2 x 477

kW

2 x 640

SHP

Maximum continuous power

2 x 423

kW

2 x 567

SHP

O.E.I. Max contingency (2.5 min)

546

kW

732

SHP

O.E.I. Max continuous power

500

kW

670

SHP

Engine Rating (2 x Turbomeca Arrius 2K-1)

Take Off power (5 min)

2 x 500

kW

2 x 670

SHP

Maximum continuous power

2 x 425

kW

2 x 570

SHP

O.E.I. Max contingency (2.5 min)

560

kW

750

SHP

O.E.I. Max continuous power

500

kW

670

SHP

Transmission Rating

Take Off power (5 min)

671

kW

900

SHP

Maximum continuous power

671

kW

900

SHP

O.E.I. Max contingency (2.5 min)

477

kW

640

SHP

O.E.I. Max continuous power

417

kW

560

SHP

Fuel Capacity

3 cell fuel system

605

l

160

USG

4 cell fuel system

710

l

188

USG

5 cell fuel system

870

l

230

USG

Crew

Pilot / Passengers

1 / 7

†

†

†

External Dimensions

Length (rotors turning)

13,04

m

42,78

ft

Length (rotors stopped)

11,45

m

37,59

ft

Width (rotor blades at 45∞)

7,78

m

25,53

ft

Maximum height

3,50

m

11,48

ft

Main rotor diameter

11,00

m

36,09

ft

Tail rotor diameter

2,00

m

6,56

ft

MR tip blade ground clearance

2,45

m

8,04

ft

Belly ground clearance

0,40

m

1,31

ft

Cabin floor height

0,42

m

1,38

ft

Performance (ISA, 2850 kg / 6283 lb)